This App is Generally used to analyse the Fixed Wing Unmanned UAV.
LONGITUDINAL STABILITY
Assumption made during the stability analysis
• We assume that there exists a plane of symmetry about which the geometry is symmetric and also mass distribution.
• The longitudinal control will not generate any lateral or directional forces and moments and vice versa,
• Aerodynamic forces and moments vary linearly wing angle of attack.
• We will use principle of superposition.
引用格式
RAHUL N (2024). UAV LONGITUDINAL STABILITY (https://www.mathworks.com/matlabcentral/fileexchange/124825-uav-longitudinal-stability), MATLAB Central File Exchange. 检索来源 .
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R2022b
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